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Results: 1 through 50 of 139 (0.347 secs)
You searched for: publisher:"Washington, D.C. : NACA"
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[texts]On the design of airfoils in which the transition of the boundary layer is delayed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778659&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar flow; Aerofoils
Downloads: 126
[texts]On the turbulent friction layer for rising pressure - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779898&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 189
[texts]Exploratory investigation of transpiration cooling of a 40° double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295° to 2,910° F - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853034&ix=nu&I=0&V=D&pm=1
Keywords: Transpiration (Physics; Aerodynamics--Research
Downloads: 50
[texts]Comparison of the experimental and theoretical distributions of lift on a slender inclined body of revolution at M = 2 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854796&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Laminar boundary layer--Research; Aerodynamics--Research
Downloads: 77
[texts]Jet diffusion in proximity of a wall - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804195&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet engines
Downloads: 130
[texts]Generalization of Joukowski formula to an airfoil of a cascade in compressible gas stream with subsonic velocities - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779967&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Aerofoils
Downloads: 143
[texts]Heat transfer, diffusion and evaporation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780007&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Heat--Transmission
Downloads: 130
[texts]Nonlinear theory of a hot-wire anemometer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778597&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Hot-wire anemometer
Downloads: 113
[texts]Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808552&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Triangular; Fighter planes--Wings--Testing; Aerodynamics--Research
Downloads: 74
[texts]Method for simulating the atmospheric entry of long-range ballistic missiles - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853027&ix=nu&I=0&V=D&pm=1
Keywords: Ballistic missiles--Atmospheric entry; Aerodynamics--Research
Downloads: 104
[texts]Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003833712&ix=nu&I=0&V=D&pm=1
Keywords: Research aircraft; Aerodynamics--Research
Downloads: 111
[texts]Behavior of the laminar boundary layer for periodically oscillating pressure variation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759951&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 172
[texts]Infinitesimal conical supersonic flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780782&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Differential equations
Downloads: 145
[texts]On combustion in a turbulent flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780780&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 171
[texts]New simple interferometer for obtaining quantitatively evaluable flow patterns - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780275&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Interferometers
Downloads: 81
[texts]Note on the importance of imperfect-gas effects and variation of heat capacities on the isentropic flow of gases - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810749&ix=nu&I=0&V=D&pm=1
Keywords: Isentropic expansion; Gases, Real; Aerodynamics--Research
Downloads: 111
[texts]Turbulence in the wake of a thin airfoil at low speeds - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875247&ix=nu&I=0&V=D&pm=1
Keywords: Downwash (Aerodynamics; Airplanes--Wings--Testing
Downloads: 225
[texts]Summary of information on support interference at transonic and supersonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808466&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Aerodynamics, Supersonic
Downloads: 114
[texts]On stability and turbulence of fluid flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003764328&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulence
Downloads: 195
[texts]Calculation of the shape of a two-dimensional supersonic nozzle in closed form - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778681&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic nozzles
Downloads: 201
[texts]Remark on the theory of lifting surfaces - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807494&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 57
[texts]On the problem of gas flow over an infinite cascade using Chaplygin's approximation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874033&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 78
[texts]Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810742&ix=nu&I=0&V=D&pm=1
Keywords: Thermocouples; Aerodynamics--Research
Downloads: 96
[texts]Drag reduction by suction of the boundary layer separated behind shock wave formation at high mach numbers - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760239&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Boundary layer
Downloads: 95
[texts]Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number of 1.5 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810752&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Drag (Aerodynamics; Aerodynamics--Research
Downloads: 49
[texts]Extension to the cases of two dimensional and spherically symmetric flows of two particular solutions to the equations of motion governing unsteady flow in a gas - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875517&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors; Gas flow--Research
Downloads: 74
[texts]Resistance of cascade of airfoils in gas stream at subsonic velocity - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779974&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics; Laminar boundary layer
Downloads: 93
[texts]Laminar flow about a rotating body of revolution in an axial airstream - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874362&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer; Rotational motion (Rigid dynamics
Downloads: 100
[texts]Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810536&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cooling; Aerodynamics--Research
Downloads: 105
[texts]Theoretical analysis of stationary potential flows and boundary layers at high speed =: Theoretische untersuchungen über stationäre potentialströmungen und grenzschichten bei hohen geschwindigkeiten - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003604221&ix=nu&I=0&V=D&pm=1
Keywords: Gas dynamics; Laminar boundary layer; Aerodynamics--Research
Downloads: 76
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 180
[texts]Effect of the acceleration of enlongated bodies of revolution upon the resistance in a compressible flow - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759947&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Two-body problem; Aerodynamics; Unsteady flow (Aerodynamics
Downloads: 102
[texts]Concerning the flow about ring-shaped cowlings of finite thickness: Part I - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779497&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors--Cowlings
Downloads: 64
[texts]Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310° and 3,500° R on a magnesium fin with several leading-edge modifications - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853254&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research; Magnesium--Electrometallurgy
Downloads: 99
[texts]Heat transfer by free convection from horizontal cylinders in diatomic gases - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780141&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 93
[texts]Compression shocks in two-dimensional gas flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804321&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Shock waves
Downloads: 160
[texts]On the range of applicability of the transonic area rule - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808573&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Triangular; Aerodynamics, Transonic; Aerodynamics--Research
Downloads: 98 4.00 out of 5 stars4.00 out of 5 stars4.00 out of 5 stars4.00 out of 5 stars(1 review)
[texts]Lift on a bent, flat plate - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778991&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Wings
Downloads: 192
[texts]Autogenous welding in airplane construction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874350&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Design and construction; Oxyacetylene welding and cutting
Downloads: 233
[texts]Nonstationary gas flow in thin pipes of variable cross section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804176&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Difference equations; Gas flow
Downloads: 158
[texts]Formation of a vortex at the edge of a plate - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874042&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 73
[texts]Temperature recovery factors on a slender 12° cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45° - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854733&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Laminar boundary layer--Research; Aerodynamics--Research
Downloads: 91
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 69
[texts]Experimental study of flow past turbine blades - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804235&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas-turbines
Downloads: 87
[texts]Theoretical investigation of drag reduction in maintaining the laminar boundary layer by suction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780451&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Laminar boundary layer
Downloads: 171
[texts]Correlation of supersonic convective heat-transfer coefficients from measurements of the skin temperature of a parabolic body of revolution (NACA RM-10) - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810614&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Aerodynamics--Research
Downloads: 86
[texts]Concerning the flow about ring-shaped cowlings.: Part XIII, the influence of a projecting hub - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003769590&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet engines--Air intakes
Downloads: 91
[texts]General solutions of optimum problems in nonstationary flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807493&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Flight testing; Aerodynamics--Research
Downloads: 77
[texts]Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808103&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Nusselt number; Aerodynamics--Research
Downloads: 202
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 81
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